- Design and development
- Specifications (S)
- References
| name=S | image= | caption= }}{{Infobox Aircraft Type | type=Paramotor | national origin=France | manufacturer=Reflex Paramoteur | designer=Dominique Cholou | first flight= | introduced= | retired= | status=Production completed | primary user= | more users= | produced= | number built= | program cost= | unit cost= €3,160 (2004) | developed from= | variants with their own articles=
}} |
The Reflex S is a French paramotor that was designed by Dominique Cholou and produced by Reflex Paramoteur of Chatou for powered paragliding. Now out of production, when it was available the aircraft was supplied complete and ready-to-fly.[1] Design and developmentThe "S" was designed to comply with the European microlight regulations. It features a paraglider-style wing, single-place accommodation and a single Simonini Racing {{convert|25|hp|kW|0|abbr=on}} engine in pusher configuration with a 2.38:1 ratio reduction drive and a {{convert|115|cm|in|0|abbr=on}} or {{convert|123|cm|in|0|abbr=on}} diameter three-bladed composite propeller. The fuel tank capacity is {{convert|10|l}}.[1] As is the case with all paramotors, take-off and landing is accomplished by foot. Inflight steering is accomplished via handles that actuate the canopy brakes, creating roll and yaw.[1] Specifications (S) {{Aircraft specs
|ref=Bertrand[1]
|prime units?=met
|genhide=
|crew=one
|capacity=
|length m=
|length ft=
|length in=
|length note=
|span m=
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=27
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|10|l}}
|more general=
|eng1 number=1
|eng1 name=Simonini Racing
|eng1 type=single cylinder, two-stroke, air-cooled aircraft engine, with a 2.38:1 reduction drive
|eng1 kw=
|eng1 hp=25
|prop blade number=3
|prop name=composite, ground adjustable
|prop dia m=1.23
|prop dia ft=
|prop dia in=
|prop note=
|perfhide=Y
|max speed kmh=
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=
|range miles=
|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}
References1. ^1 2 3 Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 74. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X
{{Reflex aircraft}} 4 : Reflex aircraft|French ultralight aircraft 2000–2009|Single-engined pusher aircraft|Paramotors |